US7981137B2 - Uniform stress needle - Google Patents
Uniform stress needle Download PDFInfo
- Publication number
- US7981137B2 US7981137B2 US11/415,740 US41574006A US7981137B2 US 7981137 B2 US7981137 B2 US 7981137B2 US 41574006 A US41574006 A US 41574006A US 7981137 B2 US7981137 B2 US 7981137B2
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- US
- United States
- Prior art keywords
- needle
- end section
- distal end
- section
- distal
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related, expires
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- 238000005452 bending Methods 0.000 description 11
- 230000035515 penetration Effects 0.000 description 6
- 230000001747 exhibiting effect Effects 0.000 description 2
- 230000002349 favourable effect Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 238000012079 reconstructive surgical procedure Methods 0.000 description 1
- 238000001356 surgical procedure Methods 0.000 description 1
Images
Classifications
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61B—DIAGNOSIS; SURGERY; IDENTIFICATION
- A61B17/00—Surgical instruments, devices or methods
- A61B17/04—Surgical instruments, devices or methods for suturing wounds; Holders or packages for needles or suture materials
- A61B17/06—Needles ; Sutures; Needle-suture combinations; Holders or packages for needles or suture materials
- A61B17/06066—Needles, e.g. needle tip configurations
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61B—DIAGNOSIS; SURGERY; IDENTIFICATION
- A61B17/00—Surgical instruments, devices or methods
- A61B2017/00831—Material properties
- A61B2017/0084—Material properties low friction
- A61B2017/00849—Material properties low friction with respect to tissue, e.g. hollow organs
Definitions
- the present disclosure relates to surgical needles and, more particularly to surgical needles having a distal taper exhibiting a substantially uniform stress profile which is resistant to a bending load applied thereto.
- Surgical suture needles are well known in the medical arts and include primarily two types of needles, taper point type needles and cutting edge type needles.
- a taper point type surgical needle includes a proximal end portion defining a suture-mounting portion having a hole or channel to which a suture is to be attached, an intermediate portion defining a main body portion having a generally uniform cross-sectional area throughout an entire length thereof, and a distal end portion defining a tapered portion whose cross-sectional area decreases progressively toward a pointed distal end of the suture needle.
- Cutting edge type needles also taper to a piercing point, however, unlike taper point type needles, cutting edge type needles include one or more cutting edges with an otherwise smooth outer surface.
- the needles In the design of either taper point type or cutting edge type surgical needles it is generally desirable for the needles to exhibit favorable strength and ease of penetration characteristics. It is desirable for a surgical needle to be sufficiently strong in order to penetrate tissue which is being sutured without bending or breaking during a surgical procedure. It is also desirable for the surgical needle to easily penetrate and smoothly pass through the tissue being sutured.
- the amount of force required for the surgical needle to penetrate tissue includes the force required for the engagement of the tip of the needle with the tissue and the subsequent creation of the entry hole as well as the force required for the widening of the entry hole created.
- the force required for a taper point type surgical needle to widen the hole is greater than the force required for a cutting edge type needle since the taper point type needle merely dilates the hole and does not cut the hole as would a cutting edge type needle.
- Taper point type surgical needles typically have a taper from a middle section of the needle body which ends in a distal piercing point.
- the taper is often expressed as a ratio of the length of the taper section to the diameter of the wire used to form the needle. It is known that the higher the taper ratio is, the more slender the taper, and thus the resistance to penetration and/or piercing through tissue will typically be lessened. However, the more slender the taper, the mechanical strength for needles manufactured from the same material will be lessened. The converse is also to be expected for needles having lower taper ratios.
- the piercing resistance which the suture needle receives from the tissue of the living body is at a maximum level when the surgical needle is first piercing the skin of the tissue. This is due to the fact that the skin of the tissue has a greater rupture strength than the other parts or layers of the tissue.
- the resistance of the suture needle as the needle pierces through the skin of the tissue greatly depends on the degree of sharpness of the pointed end of the suture needle. Once the suture needle pierces the skin of the tissue, the piercing resistance is abruptly reduced regardless of the value of the cross-sectional area increase rate of the tapered portion.
- one approach to improve the strength of a needle is to increase the diameter or thickness of the needle.
- the force necessary to penetrate the tissue is also increased, and the opening left in the tissue after passage of the needle is also enlarged.
- ease of penetration can be improved by making the needle thinner or more slender.
- a reduction in the thickness of the needle will generally result in a corresponding reduction in the strength of the needle.
- the present disclosure is directed to a surgical needle having a distal end taper or parabolic profile which exhibits a substantially uniform stress profile when subjected to a load to resist bending thereof.
- the surgical needle is intended for use in suturing delicate tissue in conjunction with a plastic, ophthalmologic or reconstructive surgical procedure.
- the surgical needle includes a taper point profile designed to function as a uniform stress beam and resist bending loads applied to the needle end.
- the taper point profile is defined by having cross-section diameters which dynamically increase over the length of the needle end. More specifically, the taper point profile of the uniform stress type needle defines a varied taper angle along the length of the needle end with the taper angle decreasing at locations away from the needle point.
- the taper angles, particularly, adjacent the needle end of the uniform stress type needle are typically substantially greater than corresponding taper angles of a conventional continuous taper point type needle.
- the uniform stress type needle defines an enlarged taper point profile relative to conventional taper point type needles. Consequently, the uniform stress type needle is desirably more resistant to breakage.
- the cross-section diameters of the taper point profile of the uniform stress type needle are calculated at distances from the needle point using a predetermined maximum allowable stress value.
- the formula employed for calculating section diameters of the taper point profile is derived from the universal formula for bending stress in a tip loaded cantilever beam.
- the bending stress at a location along a cantilever beam is directly related to the bending moment and sectional properties at the particular location.
- Diameters are calculated as a function of the maximum allowable bending stress and the distance from the needle point at specific locations along the taper point profile.
- the formula for the desired maximum bending stress for circular section properties, and the formula for the bending moment are combined into a formula defining the diameters along the length of a tip loaded round section tapering beam.
- the various diameters calculated create a taper point profile which effectively functions as a uniform stress beam.
- An exception is made in the area or region up to one wire diameter from the needle point to permit a sharper tip angle.
- a surgical needle having a linear body portion including a proximal end section; a central section; and a distal end section.
- the distal end section has a substantially parabolic configuration for producing a substantially uniform stress profile along a length thereof.
- the distal end section has a diameter determined according to the equation provided above.
- the distal end section includes a distal tip having a uniform taper.
- the distal tip can have a length which is substantially equal to a diameter of the central section of the surgical needle.
- proximal end section is configured and adapted to secure a suture thereto.
- the central section can have a rectilinear, circular, oval, triangular, I-beam and/or ribbon shaped cross-sectional profile.
- a uniform stress needle includes a proximal end section configured and adapted to secure a suture thereto; a central section having a uniform transverse cross-sectional profile; and a distal end section having a parabolic surface profile for producing a substantially uniform stress along a length thereof.
- the surface profile of the distal end section is defined by the equation provided above.
- the distal end section includes a distal tip having a uniform taper.
- the distal tip preferably has a length which is substantially equal to a diameter of the central section of the needle.
- a surgical needle including a body portion having a proximal end section; a central section; and a distal end section.
- the distal end section has a substantially parabolic configuration for producing a substantially uniform stress profile along a length thereof.
- the distal end section includes a distal tip having a uniform taper.
- FIG. 1 is a perspective view of a surgical needle in accordance with the present invention
- FIG. 2 is a side elevational view of a distal end of the surgical needle shown in FIG. 1 ;
- FIG. 3 is a schematic side elevational view of the surgical needle shown in FIG. 1 illustrated as a cantilevered beam;
- FIG. 4 is a schematic side elevational view of the surgical needle shown in FIG. 1 illustrating the application of a load force at a distal end thereof.
- distal refers to that portion which is further from the user
- proximal refers to that portion which is closer to the user
- Surgical needle 100 includes a linear body portion 102 having a proximal end section 110 , a distal end section 120 and a central section 130 .
- FIG. 1 illustrates a straight point type surgical needle, it will be appreciated by those skilled in the art that surgical needle 100 may have other conventional curvatures including compound, 1 ⁇ 4, 3 ⁇ 8, 1 ⁇ 2 or 5 ⁇ 8 type curvatures.
- proximal end section 110 is configured and adapted to receive and hold a surgical suture 112 therein or therethrough.
- central section 130 is shown as having a generally rectangular and/or rectilinear cross-section, it is contemplated that central section 130 may have other conventional configurations including circular, oval, triangular, I-beam, ribbon and the like.
- the cross-sectional profile should be such that a conventional needle grasper can sufficiently grasp and effectively maintain surgical needle 100 in a fixed position as surgical needle 100 penetrates body tissue, thereby preventing the needle from slipping between the jaws of the needle grasper. It is contemplated that central section 130 has a uniform transverse cross-sectional profile.
- distal end section 120 of surgical needle 100 has a substantially parabolic surface profile for producing a substantially uniform stress profile along its length.
- the longitudinal cross-sectional profile of distal end section 120 of surgical needle 100 will exhibit a curvature defined by the diametrical equation above. Accordingly, by manufacturing distal end section 120 of surgical needle 100 in accordance with the above diametric equation, distal end section 120 of surgical needle 100 will experience a substantially uniform stress profile along its length.
- distal end section 120 experiences a substantially uniform stress at each location X n along its length thereby defining a substantially uniform stress profile along its entire length thereof.
- distal end section 120 of surgical needle 100 includes a distal tip 122 having a profile which defines a tip having a sharper angle than the tip defined by the diametrical equation presented above.
- distal tip 122 has a uniform taper (i.e., a uniform and/or a non-parabolic surface profile).
- the sharper angle of distal tip 122 has a length which is substantially equal to one wire diameter (i.e., the diameter of the intermediate body portion of surgical needle).
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- Health & Medical Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Surgery (AREA)
- Heart & Thoracic Surgery (AREA)
- Engineering & Computer Science (AREA)
- Biomedical Technology (AREA)
- Nuclear Medicine, Radiotherapy & Molecular Imaging (AREA)
- Medical Informatics (AREA)
- Molecular Biology (AREA)
- Animal Behavior & Ethology (AREA)
- General Health & Medical Sciences (AREA)
- Public Health (AREA)
- Veterinary Medicine (AREA)
- Surgical Instruments (AREA)
- Infusion, Injection, And Reservoir Apparatuses (AREA)
Abstract
Description
d 3=[(32W)/(πσ)]*(X n)
where
-
- d=measured diameter at location Xn;
- W=load normal to the needle;
- Xn=distance from a distal-most end of the needle; and
- σ=chosen stress restraint.
d=(((32W)/(πσ))*(X n))^(⅓)
where
-
- d=measured diameter at location Xn;
- W=load normal to the needle;
- Xn=distance from a distal-most end of the needle; and
- σ=chosen stress restraint.
-
- Length of the distal end section of the surgical needle=0.3 inches;
- Stress=σ=145,000 p.s.i.; and
- Tip Load=W=35 grams at 45° or 0.077 lbs at 45°.
Distance from Tip | Distance from Tail | Diameter |
0.001 | 0.299 | 0.0015548 |
0.002 | 0.298 | 0.0019589 |
0.003 | 0.297 | 0.0022424 |
0.004 | 0.296 | 0.0024681 |
0.005 | 0.295 | 0.0026587 |
0.006 | 0.294 | 0.0028253 |
0.007 | 0.293 | 0.0029742 |
0.008 | 0.292 | 0.0031096 |
0.009 | 0.291 | 0.0032341 |
0.010 | 0.290 | 0.0033497 |
0.011 | 0.289 | 0.0034579 |
0.012 | 0.288 | 0.0035596 |
0.013 | 0.287 | 0.0036559 |
0.014 | 0.286 | 0.0037473 |
0.015 | 0.285 | 0.0038345 |
0.016 | 0.284 | 0.0039179 |
0.017 | 0.283 | 0.0039978 |
0.018 | 0.282 | 0.0040747 |
0.019 | 0.281 | 0.0041488 |
0.020 | 0.280 | 0.0042204 |
0.021 | 0.279 | 0.0042896 |
0.022 | 0.278 | 0.0043566 |
0.023 | 0.277 | 0.0044217 |
0.024 | 0.276 | 0.0044848 |
0.025 | 0.275 | 0.0045463 |
0.026 | 0.274 | 0.0046061 |
0.027 | 0.273 | 0.0046644 |
0.028 | 0.272 | 0.0047213 |
0.029 | 0.271 | 0.0047769 |
0.030 | 0.270 | 0.0048311 |
0.031 | 0.269 | 0.0048842 |
0.032 | 0.268 | 0.0049362 |
0.033 | 0.267 | 0.0049871 |
0.034 | 0.266 | 0.0050370 |
0.035 | 0.265 | 0.0050859 |
0.036 | 0.264 | 0.0051339 |
0.037 | 0.263 | 0.0051810 |
0.038 | 0.262 | 0.0052272 |
0.039 | 0.261 | 0.0052727 |
0.040 | 0.260 | 0.0053174 |
0.041 | 0.259 | 0.0053613 |
0.042 | 0.258 | 0.0054045 |
0.043 | 0.257 | 0.0054471 |
0.044 | 0.256 | 0.0054890 |
0.045 | 0.255 | 0.0055303 |
0.046 | 0.254 | 0.0055709 |
0.047 | 0.253 | 0.0056110 |
0.048 | 0.252 | 0.0056505 |
0.049 | 0.251 | 0.0056895 |
0.050 | 0.250 | 0.0057280 |
0.051 | 0.249 | 0.0057659 |
0.052 | 0.248 | 0.0058033 |
0.053 | 0.247 | 0.0058403 |
0.054 | 0.246 | 0.0058768 |
0.055 | 0.245 | 0.0059129 |
0.056 | 0.244 | 0.0059485 |
0.057 | 0.243 | 0.0059837 |
0.058 | 0.242 | 0.0060185 |
0.059 | 0.241 | 0.0060529 |
0.060 | 0.240 | 0.0060869 |
0.061 | 0.239 | 0.0061205 |
0.062 | 0.238 | 0.0061538 |
0.063 | 0.237 | 0.0061867 |
0.064 | 0.236 | 0.0062192 |
0.065 | 0.235 | 0.0062514 |
0.066 | 0.234 | 0.0062833 |
0.067 | 0.233 | 0.0063149 |
0.068 | 0.232 | 0.0063462 |
0.069 | 0.231 | 0.0063771 |
0.070 | 0.230 | 0.0064078 |
0.071 | 0.229 | 0.0064382 |
0.072 | 0.228 | 0.0064683 |
0.073 | 0.227 | 0.0064981 |
0.074 | 0.226 | 0.0065276 |
0.075 | 0.225 | 0.0065569 |
0.076 | 0.224 | 0.0065859 |
0.077 | 0.223 | 0.0066146 |
0.078 | 0.222 | 0.0066432 |
0.079 | 0.221 | 0.0066714 |
0.080 | 0.220 | 0.0066995 |
0.081 | 0.219 | 0.0067273 |
0.082 | 0.218 | 0.0067548 |
0.083 | 0.217 | 0.0067822 |
0.084 | 0.216 | 0.0068093 |
0.085 | 0.215 | 0.0068362 |
0.086 | 0.214 | 0.0068629 |
0.087 | 0.213 | 0.0068894 |
0.088 | 0.212 | 0.0069157 |
0.089 | 0.211 | 0.0069418 |
0.090 | 0.210 | 0.0069677 |
0.091 | 0.209 | 0.0069934 |
0.092 | 0.208 | 0.0070189 |
0.093 | 0.207 | 0.0070443 |
0.094 | 0.206 | 0.0070694 |
0.095 | 0.205 | 0.0070944 |
0.096 | 0.204 | 0.0071192 |
0.097 | 0.203 | 0.0071439 |
0.098 | 0.202 | 0.0071683 |
0.099 | 0.201 | 0.0071926 |
0.100 | 0.200 | 0.0072168 |
0.101 | 0.199 | 0.0072407 |
0.102 | 0.198 | 0.0072646 |
0.103 | 0.197 | 0.0072882 |
0.104 | 0.196 | 0.0073117 |
0.105 | 0.195 | 0.0073351 |
0.106 | 0.194 | 0.0073583 |
0.107 | 0.193 | 0.0073814 |
0.108 | 0.192 | 0.0074043 |
0.109 | 0.191 | 0.0074271 |
0.110 | 0.190 | 0.0074497 |
0.111 | 0.189 | 0.0074722 |
0.112 | 0.188 | 0.0074946 |
0.113 | 0.187 | 0.0075168 |
0.114 | 0.186 | 0.0075390 |
0.115 | 0.185 | 0.0075609 |
0.116 | 0.184 | 0.0075828 |
0.117 | 0.183 | 0.0076045 |
0.118 | 0.182 | 0.0076261 |
0.119 | 0.181 | 0.0076476 |
0.120 | 0.180 | 0.0076690 |
Claims (5)
d=(((32W)/(πσ))*(X n))^(⅓)
d=(((32W)/(πσ))*(X n))^(⅓),
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/415,740 US7981137B2 (en) | 2002-07-17 | 2006-05-01 | Uniform stress needle |
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US39637602P | 2002-07-17 | 2002-07-17 | |
US39694102P | 2002-07-17 | 2002-07-17 | |
US10/620,160 US7063716B2 (en) | 2002-07-17 | 2003-07-15 | Uniform stress needle |
US10/993,544 US7059510B2 (en) | 2002-05-31 | 2004-11-19 | End-to-end anastomosis instrument and method for performing same |
US11/415,740 US7981137B2 (en) | 2002-07-17 | 2006-05-01 | Uniform stress needle |
Related Parent Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US10/620,160 Continuation US7063716B2 (en) | 2002-07-17 | 2003-07-15 | Uniform stress needle |
US10/993,544 Continuation US7059510B2 (en) | 2002-05-31 | 2004-11-19 | End-to-end anastomosis instrument and method for performing same |
Publications (2)
Publication Number | Publication Date |
---|---|
US20060195141A1 US20060195141A1 (en) | 2006-08-31 |
US7981137B2 true US7981137B2 (en) | 2011-07-19 |
Family
ID=30116080
Family Applications (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US10/620,160 Expired - Fee Related US7063716B2 (en) | 2002-07-17 | 2003-07-15 | Uniform stress needle |
US10/621,759 Expired - Fee Related US7179277B2 (en) | 2002-07-17 | 2003-07-17 | Surgical needle |
US11/415,740 Expired - Fee Related US7981137B2 (en) | 2002-07-17 | 2006-05-01 | Uniform stress needle |
Family Applications Before (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US10/620,160 Expired - Fee Related US7063716B2 (en) | 2002-07-17 | 2003-07-15 | Uniform stress needle |
US10/621,759 Expired - Fee Related US7179277B2 (en) | 2002-07-17 | 2003-07-17 | Surgical needle |
Country Status (6)
Country | Link |
---|---|
US (3) | US7063716B2 (en) |
EP (1) | EP1545326B1 (en) |
AU (1) | AU2003256541A1 (en) |
CA (1) | CA2491042C (en) |
ES (1) | ES2385557T3 (en) |
WO (1) | WO2004006988A2 (en) |
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Also Published As
Publication number | Publication date |
---|---|
AU2003256541A1 (en) | 2004-02-02 |
WO2004006988A2 (en) | 2004-01-22 |
CA2491042A1 (en) | 2004-01-22 |
CA2491042C (en) | 2011-01-25 |
US20040059379A1 (en) | 2004-03-25 |
AU2003256541A8 (en) | 2004-02-02 |
EP1545326A2 (en) | 2005-06-29 |
WO2004006988A3 (en) | 2004-06-24 |
EP1545326A4 (en) | 2010-06-09 |
ES2385557T3 (en) | 2012-07-26 |
US7179277B2 (en) | 2007-02-20 |
EP1545326B1 (en) | 2012-05-30 |
US20040059380A1 (en) | 2004-03-25 |
US7063716B2 (en) | 2006-06-20 |
US20060195141A1 (en) | 2006-08-31 |
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